BE460696A - - Google Patents
Info
- Publication number
- BE460696A BE460696A BE460696DA BE460696A BE 460696 A BE460696 A BE 460696A BE 460696D A BE460696D A BE 460696DA BE 460696 A BE460696 A BE 460696A
- Authority
- BE
- Belgium
- Prior art keywords
- turbine
- compressor
- chambers
- air
- combustion
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims description 41
- 239000007789 gas Substances 0.000 claims description 22
- 239000000446 fuel Substances 0.000 claims description 11
- 230000002146 bilateral effect Effects 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 4
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 239000007788 liquid Substances 0.000 claims description 2
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 239000000567 combustion gas Substances 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000009826 distribution Methods 0.000 description 3
- 238000005192 partition Methods 0.000 description 3
- 230000008016 vaporization Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000004087 circulation Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- CDMADVZSLOHIFP-UHFFFAOYSA-N disodium;3,7-dioxido-2,4,6,8,9-pentaoxa-1,3,5,7-tetraborabicyclo[3.3.1]nonane;decahydrate Chemical compound O.O.O.O.O.O.O.O.O.O.[Na+].[Na+].O1B([O-])OB2OB([O-])OB1O2 CDMADVZSLOHIFP-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000009827 uniform distribution Methods 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000006200 vaporizer Substances 0.000 description 1
- 210000001835 viscera Anatomy 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE460696A true BE460696A (de) |
Family
ID=113507
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE460696D BE460696A (de) |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE460696A (de) |
-
0
- BE BE460696D patent/BE460696A/fr unknown
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3155234B1 (de) | Turbinenmotor mit einem antriebssystem für eine vorrichtung wie ein hilfsaggregatgehäuse | |
| FR2616886A1 (fr) | Chambre de combustion annulaire pour une turbine a gaz | |
| CA3044563C (fr) | Turbomachine, notamment turbogenerateur et echangeur pour une telle turbomachine | |
| CH422137A (fr) | Machine dynamo-électrique refroidie par un liquide | |
| FR2692627A1 (fr) | Ensemble de carters de compresseur, installation de prélèvement d'air pour ceux-ci et procédé de régulation de la distorsion de cet ensemble de carters. | |
| FR2968353A1 (fr) | Buse de diffusion a etagement d'air | |
| BE461566A (de) | ||
| EP1770333B1 (de) | Anti-Verkokungsinjektorarm | |
| EP3504481B1 (de) | Brennkammer mit einem deflektor für verdichtete heissluft, insbesondere für eine turbine zur erzeugung von energie, insbesondere von elektrischer energie | |
| BE460696A (de) | ||
| EP3447271B1 (de) | Heizsystem für sekundäre düse vom konvergierenden/divergierenden typ | |
| EP4720484A1 (de) | Flugzeugturbinentriebwerk mit wiedergewonnenem zyklus | |
| FR3080652A1 (fr) | Turbomachine a architecture inversee, optionnellement pourvue d'un recuperateur de chaleur en sortie de turbine basse pression | |
| BE478436A (de) | ||
| BE674852A (de) | ||
| EP3830486A1 (de) | Brennkammer mit einem durchgangsabschnitt eines flammrohrs, das modifiziert ist; insbesondere für eine turbine zur erzeugung von leistung, insbesondere elektrischem strom | |
| FR3084448A1 (fr) | Chambre de combustion pour une turbine a gaz destinee a la production d'energie notamment d'energie electrique, comprenant des trous de dilution orientes dans un tube a flamme. | |
| EP3504480B1 (de) | Modulare turbine mit wärmetauscher zur erzeugung von elektrischer energie | |
| FR3167174A1 (fr) | Turbomachine equipee d’une machine electrique et d’un dispositif de refroidissement | |
| BE480889A (de) | ||
| FR3164252A1 (fr) | Système de trains épicycloïdaux pour turbomachine et turbomachine comprenant un tel système | |
| FR3162832A1 (fr) | Dispositif de tourbillonnement radial pour chambre de combustion de turbomachine. | |
| FR3162831A1 (fr) | Dispositif de tourbillonnement axial pour chambre de combustion de turbomachine. | |
| WO2024175849A1 (fr) | Systeme d'echange de chaleur pour une turbomachine d'aeronef | |
| BE463343A (de) |